CN204279980U - A kind of suspended beam type wing movable part center position clamp structure - Google Patents

A kind of suspended beam type wing movable part center position clamp structure Download PDF

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Publication number
CN204279980U
CN204279980U CN201420756635.XU CN201420756635U CN204279980U CN 204279980 U CN204279980 U CN 204279980U CN 201420756635 U CN201420756635 U CN 201420756635U CN 204279980 U CN204279980 U CN 204279980U
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China
Prior art keywords
clamp
wing
movable part
drop
center position
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CN201420756635.XU
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Chinese (zh)
Inventor
杨阳
邱燕平
杰小平
黄金金
黄启湘
曹青霞
杨欢
吕鹂
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Priority to CN201420756635.XU priority Critical patent/CN204279980U/en
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Abstract

The utility model relates to aircraft manufacturing field, is specifically related to a kind of suspended beam type wing movable part center position clamp structure.Comprise clamp, drop in beam hole locator, drop in beam hole latch, bolt, the shape of clamp is tabular, it is while the Contour matching of the fixed parts that hollows out with wing and movable part, and drop in beam hole locator is bolted on clamp, and drop in beam hole latch can insert to be in drop in beam hole locator.Clamp is provided with some boss for the laminating between clamp and the fixed parts of wing.Also process gasket is provided with between boss and the fixed parts of wing.The utility model designs simplification, rationally, use which solves wing movable part center position adjustment problem, not only version is succinct, be convenient to manufacture, operate, effectively can reduce technological preparation time, movable part center position regulation time, also because it has adjustment function by process gasket, compensate the center position alignment error that wing fixed parts skin shape error is brought.

Description

A kind of suspended beam type wing movable part center position clamp structure
Technical field
The utility model relates to aircraft manufacturing field, is specifically related to a kind of suspended beam type wing movable part center position clamp structure.
Background technology
The adjustment of aircraft wing movable part center position generally adopts the methods such as horizontal survey point adjustment, the outer equidistant clamp of frame, measurement of angle clamp, the overall clamp of controlsurface now, these methods or special measurement instrument will be adopted, or special wing bracket will be adopted, or clamp is larger, not only need special instrument or frock operation inconvenience, also can bring measured error because of frock form, cause the problems such as the lengthening of technological preparation cycle, development cost rising, production cycle lengthening, difficult quality guarantee.
Summary of the invention
The purpose of this utility model is to solve the problem, and provides a kind of suspended beam type wing movable part center position clamp structure.
In order to realize the purpose of this utility model, the technical solution adopted in the utility model is:
A kind of suspended beam type wing movable part center position clamp structure, comprise clamp, drop in beam hole locator, drop in beam hole latch, bolt, the shape of clamp is tabular, it is while the Contour matching of the fixed parts that hollows out with wing and movable part, drop in beam hole locator is bolted on clamp, and drop in beam hole latch can insert to be in drop in beam hole locator.
Clamp is provided with some boss for the laminating between clamp and the fixed parts of wing.
Also process gasket is provided with between boss and the fixed parts of wing.
The beneficial effects of the utility model are: designs simplification, rationally, use which solves wing movable part center position adjustment problem, not only version is succinct, be convenient to manufacture, operate, effectively can reduce technological preparation time, movable part center position regulation time, also because it has adjustment function by process gasket, compensate the center position alignment error that wing fixed parts covering (wallboard) configuration error brings.
Accompanying drawing explanation
Fig. 1 is the utility model using state schematic diagram.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further illustrated:
Embodiment: see Fig. 1.
A kind of suspended beam type wing movable part center position clamp structure, comprise clamp 1, drop in beam hole locator 2, drop in beam hole latch 3, bolt 4, the shape of clamp 1 is tabular, it is while hollow out the Contour matching with the fixed parts 7 of wing and movable part 6,8, drop in beam hole locator 2 is fixed on clamp 1 by bolt 4, and drop in beam hole latch 3 can insert to be in drop in beam hole locator 2.
Clamp 1 is provided with some boss 9 for the laminating between clamp 1 and the fixed parts 7 of wing.
Process gasket 5 is also provided with between boss 9 and the fixed parts 7 of wing.
The utility model meter description of operation: when carrying out the adjustment of movable part center position, first clamp 1 is placed on solid parts 7 covering (or wallboard) of wing, fitted with covering (or wallboard) surface in boss 9 on clamp 1 surface, then clamp 1 position is adjusted, make drop in beam hole latch 3 through drop in beam hole locator 2 and the solid parts 7 drop in beam hole of wing, check the gap of solid parts 7 aerofoil of wing and clamp 1, inching is carried out by the position of process gasket 5 pairs of clamps 1 according to gap situation, ensure that fixed parts 7 aerofoil describes in poor scope to the gap of clamp 1 all outside, the now adjustment of center position clamp completes.
Then, check the gap of movable part 6 and 8 to center position clamp 1 of wing, and adjust according to gap situation movable part 6,8, movable part and clamp gap are described in poor scope all outside (as cannot to adjust to the right place, can adjust process gasket 5 in fixed-wing facial contour range of tolerable variance, movable part and clamp gap is reexamined after adjustment), be now the center position of movable part.
After adjustment, movable part 6,8 carries out center position mark, then take out drop in beam hole latch, remove center position clamp, regain process gasket, movable part center position has adjusted.
One of preferred embodiment that what embodiment of the present utility model was announced is also; but be not limited thereto; those of ordinary skill in the art; very easily according to above-described embodiment; understand spirit of the present utility model; and make different amplifications and change, but only otherwise depart from spirit of the present utility model, all in protection domain of the present utility model.

Claims (3)

1. a suspended beam type wing movable part center position clamp structure, it is characterized in that: comprise clamp, drop in beam hole locator, drop in beam hole latch, bolt, the shape of clamp is tabular, it is while the Contour matching of the fixed parts that hollows out with wing and movable part, drop in beam hole locator is bolted on clamp, and drop in beam hole latch can be inserted in drop in beam hole locator.
2. a kind of suspended beam type wing movable part center position clamp structure according to claim 1, is characterized in that: clamp is provided with some boss for the laminating between clamp and the fixed parts of wing.
3. a kind of suspended beam type wing movable part center position clamp structure according to claim 2, is characterized in that: between boss and the fixed parts of wing, be also provided with process gasket.
CN201420756635.XU 2014-12-06 2014-12-06 A kind of suspended beam type wing movable part center position clamp structure Active CN204279980U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420756635.XU CN204279980U (en) 2014-12-06 2014-12-06 A kind of suspended beam type wing movable part center position clamp structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420756635.XU CN204279980U (en) 2014-12-06 2014-12-06 A kind of suspended beam type wing movable part center position clamp structure

Publications (1)

Publication Number Publication Date
CN204279980U true CN204279980U (en) 2015-04-22

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ID=52863167

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420756635.XU Active CN204279980U (en) 2014-12-06 2014-12-06 A kind of suspended beam type wing movable part center position clamp structure

Country Status (1)

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CN (1) CN204279980U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104443429A (en) * 2014-12-06 2015-03-25 江西洪都航空工业集团有限责任公司 Suspended beam type clamping plate structure for central position of movable component of airfoil
CN105059566A (en) * 2015-08-18 2015-11-18 江西洪都航空工业集团有限责任公司 Method for detecting finish machining clamping deformation of aircraft component

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104443429A (en) * 2014-12-06 2015-03-25 江西洪都航空工业集团有限责任公司 Suspended beam type clamping plate structure for central position of movable component of airfoil
CN105059566A (en) * 2015-08-18 2015-11-18 江西洪都航空工业集团有限责任公司 Method for detecting finish machining clamping deformation of aircraft component

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